Fault-Tolerant Control of Hypersonic Vehicle Using Neural Network and Sliding Mode

In this paper, the tracking control of the air-breathing hypersonic vehicle with model parameter uncertainties and actuator faults is studied. Firstly, a high-order linearization model is used to build an adaptive terminal sliding mode that eliminates chattering and provides increased robustness for...

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Bibliographic Details
Main Authors: Peng Cui, Changsheng Gao, Wuxing Jing, Ruoming An
Format: Article
Language:English
Published: Wiley 2022-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2022/1637305
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